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| Solving Mathematical Optimization Models by Differential Equations
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Mazin Kareem Kadhim Marjan, Ahmed Sabah Aljilawi
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Abstract:
A particular emphasis will be placed on optimum control problems that are subject to differential algebraic equations, which will be the subject of this paper. It is our goal to determine the minimum power and launch time required for rockets and satellite-carrying spacecraft while maintaining the highest possible level of performance quality. Finally, the numerical results were obtained through the use of the Python programming language.
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